An apparatus for automatically controlling an aerodynamic compensation device, the one aerodynamic control is associated with surface of an aircraft

摘要

Device for the automatic control of a compensator aerodynamique9 articulated at the back of a surface aerodynamic of commande8 a 371, it - same articulee on the said 371 structure6, comprising a tringle19 articulee of a dimension in said compensator aerodynamique9 and connected to the other side to the structure6 the 371 so that a steering control of said surface aerodynamic of commande8 causes automatically the deflection of the compensator aerodynamique9 with respect to said surface aerodynamic of commande8. / p & & p & according to the invention, this device is characterizes in that, on the side opposed to the compensator aerodynamic, said tringle19 is articulee has a levier12, - same articulated on said structure6 the 371, and in that moyens14 are provided to remove the point of articulation11 the tringle19 and levier12 in a direction at least approximately transverse to said surface aerodynamique8, in connection with the steering control of said surface aerodynamic.